GB1589511A - Probe assemblies - Google Patents

Probe assemblies Download PDF

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Publication number
GB1589511A
GB1589511A GB22610/77A GB2261077A GB1589511A GB 1589511 A GB1589511 A GB 1589511A GB 22610/77 A GB22610/77 A GB 22610/77A GB 2261077 A GB2261077 A GB 2261077A GB 1589511 A GB1589511 A GB 1589511A
Authority
GB
United Kingdom
Prior art keywords
sensor head
probe
probe assembly
assembly according
probe body
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB22610/77A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Smiths Group PLC
Original Assignee
Smiths Group PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Smiths Group PLC filed Critical Smiths Group PLC
Priority to GB22610/77A priority Critical patent/GB1589511A/en
Priority to US05/909,090 priority patent/US4196390A/en
Priority to FR7815853A priority patent/FR2392364A1/en
Publication of GB1589511A publication Critical patent/GB1589511A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/42Devices characterised by the use of electric or magnetic means
    • G01P3/44Devices characterised by the use of electric or magnetic means for measuring angular speed
    • G01P3/48Devices characterised by the use of electric or magnetic means for measuring angular speed by measuring frequency of generated current or voltage
    • G01P3/481Devices characterised by the use of electric or magnetic means for measuring angular speed by measuring frequency of generated current or voltage of pulse signals
    • G01P3/486Devices characterised by the use of electric or magnetic means for measuring angular speed by measuring frequency of generated current or voltage of pulse signals delivered by photo-electric detectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/02Arrangement of sensing elements
    • F01D17/06Arrangement of sensing elements responsive to speed

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
  • Investigating Or Analyzing Materials By The Use Of Magnetic Means (AREA)

Description

PATENT SPECIFICATION
m ( 21) Application No 22610/77 ( 22) Filed 27 May 1977 lt ( 23) Complete Specification filed 26 May 1978 ( 44) Complete Specification published 13 May 1981 ( 51) INT CL 3 GO O P 1/02 ( 52) Index at acceptance GIN 1 A 2 C 1 D 3 IP 7 E 1 ( 72) Inventor JOHN EDWARD PITKIN ( 54) IMPROVEMENTS IN OR RELATING TO PROBE ASSEMBLIES ( 71) We, SMITHS INDUSTRIES LIMITED, a British Company of Cricklewood, London NW 2 6 JN, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly des-
cribed in and by the following statement:-
This invention relates to probe assemblies.
In many applications it is necessary to place a measuring or detecting sensor close to an inaccessible object or environment It is conventional in such circumstances to mount the sensor in the head of a probe assembly that can be used to position the sensor appropriately, and to secure the sensor in position by fixing the other end of the probe assembly to a mounting member Difficulties arise in such arrangements because errors in manufacture of the probe assembly or the mounting member are often magnified owing to the length of the probe body, and lead to inaccurate positioning of the sensor head Inaccurate positioning of the sensor head can also be caused by differential thermal expansion or contraction when the probe assembly is subjected to large temperature changes The displacement of the sensor head produced by temperature changes is obviously greater where the assembly is fixed at the end remote from the sensor head than would otherwise be the case, since the amount of expansion or contraction produced following a temperature change is dependent upon the length of the assembly subjected to the temperature change.
The above-mentioned difficulties can be alleviated to a certain extent if the probe assembly is resiliently secured to the mounting member at its end remote from the sensor head, such that it urges the other end of the probe assembly into contact with a locating member attached to the mounting member and positioned close to the region in which the sensor is to be placed The resilient mounting will act to accommodate to a certain extent axial displacement caused by differential thermal expansion and manufacturing errors This arrangement does however have the disadvantage that the force urging the probe assembly into contact with the locating member has to be transmitted along the entire length of the probe assembly If the probe assembly is positioned within a tube that is badly shaped, or is fouled, for example with combustion products as is often the case in gas-turbine engines, the force transmitted along the probe assembly may not be sufficient to keep the sensor head in firm contact with the locating member Another disadvantage arises where the probe assembly is subjected to vibration The sensor head, being carried by the resiliently-mounted probe body, will vibrate with the probe body and this will give rise to errors in the positioning of the sensor.
These disadvantages can be overcome by rigidly securing the probe body to the mounting member at its end remote from the sensor and resiliently mounting the sensor head on the other end of the probe body such that it is urged into contact with the locating member by its resilient mounting.
Although such an arrangement avoids to a substantial extent the problems that occur if the resilient mounting is provided between the probe body and the mounting member, it does have the added difficulty that it is necessary to form a flexible hermetic seal between the sensor head and the probe body that is capable of withstanding the hostile environment often experienced in the region of the sensor.
It is an object of the present invention to provide a probe assembly that can be used to alleviate the above-mentioned difficulties.
According to the present invention there is provided a probe assembly including a probe body; a sensor head, including sensing means, mounted at the forward end of said probe body; a sleeve member mounted with said sensor head to extend rearwardly of said sensor head; and a bellows unit sealed at its rearward end to said probe body and at its forward end to said sleeve member, wherein the forward end of the probe body ( 11) 1 589511 ( 19) 1,589,511 extends through said bellows unit and within said sleeve member, and wherein slide means is arranged resiliently to contact both the forward end of said probe body and the inner surface of said sleeve member such as to permit limited axial displacement between said probe body and said sensor head by sliding contact with said slide means.
The bellows unit may itself provide resilience between the sensor head and the probe body, or resilient means, such as, for example, a helical spring may be secured between the sensor head and the probe body to provide a major part of the resilience.
A probe assembly for measuring the speed of rotation of a shaft will now be described, by way of example, with reference to the accompanying drawing which is a partly sectional view taken on the axis of the probe assembly.
The probe assembly illustrated is especially for use in measuring the speed of rotation of a gas-turbine engine compressor shaft, but it will be appreciated that by employing sensor heads with different sensing means many other probe assemblies can be manufactured in accordance with the present invention, to measure or detect different phenomena, such as, for example, temperature Although the embodiment to be described has an electrical sensor head, the probe assembly could be easily modified to use an optical sensor head and fibre-optic cables.
The shaft-speed sensor probe assembly includes a sensor head 1 which is mounted at the forward end of a probe body 2 and which is for sensing rotation of a toothed wheel 3 mounted on the shaft (not shown) of a gas-turbine engine compressor The sensor head 1 includes a magnetic sensor of a standard form having a soft iron polepiece 4, one end of which is attached to a magnet 5 and the other end of which has an angled end-face which is arranged such that it can be brought into close proximity with the wheel 3 Two sensing coils 6 are wound around the pole-piece 4, the four ends 7 (only two of which are shown) of the coils being joined to four multistrand cables or leads 8 which serve to establish an electrically-conductive path along the length of the probe assembly The sensor head 1 has an outer generally cylindrical shell 9 of stainless-steel, that is electron-beam welded at its forward end to form a seal with the polepiece 4 The other end of the shell 9 has an annular shoulder 10 formed with an externally screw-threaded collar 11.
The sensor head 1 is resiliently interconnected with the probe body 2 by means of a helical spring 12 one end of which sits on the shoulder 10 within the collar 11 of the shell 9 The other end of the spring 12 embraces a stainless-steel bush 13 secured within one end of a stainless-steel lead-tube 14 which forms part of the probe body 2 and which extends rearwards from the sensor head 1.
A stainless-steel sleeve 15 has a forward portion 16 that surrounds the spring 12 and 70 that is screw-threaded and welded to the collar 11 of the shell 9 The sleeve 15 is also formed with a reduced diameter rear portion 17 that surrounds the forward end of the lead-tube 14 An hermetic seal is formed 75 between the sensor head 1 and the lead-tube 14 by means of a tubular bellows unit 18 that is welded at its forward end to the outside of the rear portion 17 of the sleeve 15, and at its rear end to an annular support 80 ring 19 that is in turn welded to the leadtube.
The sensor head 1 is supported axially of the lead-tube 14 by means of a spring assembly 20 made of a nimonic alloy The 85 spring assembly 20 comprises a ring 21 and four leaf springs 22 extending from the ring at positions spaced equally about it The ring 21 is brazed to the outer surface of the forward end of the lead-tube 14 with the 90 springs 22 extending rearwardly of the probe assembly and inclined outwardly away from the surface of the lead-tube Each spring 22 has an end portion 23, that is resiliently urged flat against the inner surface of the 95 rear portion 17 of the sleeve 15 The end portion 23 of each spring is free to slide over the inner surface of the sleeve 15, thereby permitting relative axial displacement between the sensor head 1 and the lead-tube 100 14 The rear portion 17 of the sleeve 15 is, however, formed at its rear end with an inturned lip 24 so as thereby to limit relative displacement of the sensor head 1 and probe body 2 away from one another by engage 105 ment with the end portion 23 of the springs 22.
The leads 8 from the sensor pass along grooves in a mild-steel guide block 25 secured to the magnet 5, and through the 110 bore of the spring 12 The leads 8 are formed into expansion loops 26 within the spring, being supported therein by a cellular silicone-rubber core 27 The leads 8 then pass through holes in the bush 13 and along 115 the lead-tube 14 where they are similarly formed into loops 28 supported by a silicone-rubber filling 29 At the rear end of the lead-tube 14 the leads are brazed to individual pins 30 of an electrical connector 120 31 that is welded to the end of the tube.
When in use, the probe assembly extends within a guide-tube 32 in the housing of the gas-turbine engine The assembly is supported within the guide-tube 32 by an '0 ' 125 ring 33 carried in a groove about the circumference of the suppor-ring 19 and by a similar support-ring 34 carrying an 'O'-ring fixed to the lead-tube 14 between the ring 19 and the connector 31 The probe assembly 130 1,589,511 is secured in position within the guide-tube 32 by bolting a flange 36 on the connector 31 to a mounting member or outer casing 37 of the engine housing The sensor head 1, at the other end of the probe assembly, passes through a hole in a plate 38 fixed in the engine housing, that acts as a locating member for positioning the end of the polepiece 4 accurately with respect to the toothed wheel 3 The length of the probe assembly is such that, when it is secured in position within the engine housing, the spring 12 and the rubber core 27 are slightly compressed, thereby urging the shoulder 10 on the sensor head 1 firmly into contact with the plate 38.
As the temperature within the engine housing changes, differential expansion occurs between the engine housing and the probe assembly, one end of which is rigidly fixed to the casing 37 This differential expansion is readily accommodated since there is resilient interconnection of the lead-tube 14 and the sensor head 1, permitting relative axial displacement between them to take place within the sleeve 15 The resilient interconnection also permits limited transverse (radial) displacement of the sensor head 1 relative to the lead-tube 14, and relative angular displacement about an axis at right angles to the lead-tube which helps accommodate for any misalignment of the plate 38 with respect to the engine casing 37 and thereby facilitates positioning of the probe assembly within the guide-tube 32.
The interconnection between the lead-tube 14 and the sensor head 1 does not, however, permit relative angular displacement about the axis of the probe assembly and thereby prevents misalignment of the angled endface of the pole-piece 4 that might otherwise arise.
The expansion loops 26 and 28 formed in the leads 8, and the silicone-rubber sup-45 port fillings 27 and 29 ensure that no damage is caused to the leads upon repeated flexing, thermal expansion and vibration.
Upon withdrawal of the probe assembly from the engine housing, the end 23 of each leaf spring 22 engages the lip 24 of the sleeve 15 and thereby prevents an excesssive tension load being applied to the bellows unit 18 In operation, the probe assembly and the guide-tube 32 often become coated with a carbon deposit which impedes withdrawal of the probe assembly, it is important therefore that the probe assembly be capable of withstanding the relatively large forces often required to remove it from the engine, without incurring any damage.

Claims (1)

  1. WHAT WE CLAIM IS: -
    1 A probe assembly including;a probe body; a sensor head, including sensing means, mounted at the forward end of said probe body; a sleeve member mounted with said sensor head to extend rearwardly of said sensor head; and a bellows unit sealed at its rearward end to said probe body and 70 at its forward end to said sleeve member, wherein the forward end of the probe body extends through said bellows unit and within said sleeve member, and wherein slide means is arranged resiliently to contact both 75 the forward end of said probe body and the inner surface of said sleeve member such as to permit limited axial displacement between said probe body and said sensor head by sliding contact with said slide means 80 2 A probe assembly according to Claim 1 wherein said bellows unit is of metal.
    3 A probe assembly according to Claim 1 or 2 including resilient means, said resilient means being arranged to provide a 85 resilient interconnection between said probe body and said sensor head.
    4 A probe assembly according to Claim 3 wherein said resilient means is a helical spring 90 A probe assembly according to any one of the preceding claims, wherein said slide means includes a spring element, said spring element being urged resiliently outwards into contact with the inner surface of 95 said sleeve.
    6 A probe assembly according to Claim 5, wherein said spring element is a leaf spring.
    7 A probe assembly according to any 100 one of the preceding claims, wherein said slide means includes a plurality of leaf springs mounted at locations spaced apart around said forward end of the probe body.
    8 A probe assembly according to any 105 one of the preceding claims, wherein said sleeve member has an inwardly-directed surface formation adapted to engage with said slide means so as thereby to limit separation of said sensor head and said probe 110 body.
    9 A probe assembly according to any one of the preceding claims including a cable for carrying signals from said sensor head, said cable extending rearwardly from the 115 sensor head through the probe body and being formed into loops so as to accommodate axial displacement between said probe body and said sensor head.
    A probe assembly according to any 120 one of the preceding claims including a cable for carrying signals from said sensor head, said cable extending rearwardly from the sensor head through the probe body and being supported along a part at least of 125 its length by a filling of resilient material.
    11 A probe assembly according to any one of the preceding claims wherein said sensor means is arranged to produce an out4 1,589,511 4 put signal in accordance with speed of rota hereinbefore described with reference to the tion of a rotatable body accompanying drawing.
    12 A probe assembly according to any one of the preceding claims wherein said For the Applicants:
    sensor head includes magnetic sensor means E SWINBANK, 13 A probe assembly substantially as Chartered Patent Agent.
    Printed for Her Majesty's Stationery Office by Burgess & Son (Abingdon), Ltd -1981 Published at The Patent Office, 25 Southampton Buildings, London, WC 2 A l AY from which copies may be obtained.
GB22610/77A 1977-05-27 1977-05-27 Probe assemblies Expired GB1589511A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB22610/77A GB1589511A (en) 1977-05-27 1977-05-27 Probe assemblies
US05/909,090 US4196390A (en) 1977-05-27 1978-05-24 Probe assembly with resiliently mounted sensor head
FR7815853A FR2392364A1 (en) 1977-05-27 1978-05-26 PROBE WITH MAGNETIC SENSOR, ESPECIALLY FOR MEASURING THE ANGULAR SPEED OF THE COMPRESSOR SHAFT OF A TURBOREACTOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22610/77A GB1589511A (en) 1977-05-27 1977-05-27 Probe assemblies

Publications (1)

Publication Number Publication Date
GB1589511A true GB1589511A (en) 1981-05-13

Family

ID=10182233

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22610/77A Expired GB1589511A (en) 1977-05-27 1977-05-27 Probe assemblies

Country Status (3)

Country Link
US (1) US4196390A (en)
FR (1) FR2392364A1 (en)
GB (1) GB1589511A (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2461950A1 (en) * 1979-07-24 1981-02-06 Radiologie Cie Gle FLEXIBLE PROBE INTENDED FOR NON-DESTRUCTIVE CONTROL OF LARGE LENGTH TUBES
US4511840A (en) * 1982-06-28 1985-04-16 Allied Corporation Mounting assembly for a speed sensor
US4563643A (en) * 1982-07-30 1986-01-07 Westinghouse Electric Corp. Eddy current proximity sensor for use in a hostile turbine environment
US4667148A (en) * 1985-06-26 1987-05-19 General Electric Company Generator air-gap flux probe for detecting shorted rotor turns
DE3523289A1 (en) * 1985-06-28 1987-01-08 Busch Dieter & Co Prueftech METHOD AND DEVICE FOR DETERMINING AND EVALUATING MACHINE CONDITION DATA
US5032790A (en) * 1987-06-01 1991-07-16 Kelsey-Hayes Company Passive magnetic speed sensor
US4833931A (en) * 1987-08-14 1989-05-30 Westinghouse Electric Corp. Thermally self-adjusting mount for proximity sensor
US6693418B2 (en) 2000-01-07 2004-02-17 Bendix Commercial Vehicle Systems Llc Magnetic wheel speed sensor having one-piece pole and magnetic flux concentrator
US20070176593A1 (en) * 2006-01-31 2007-08-02 Paul Fathauer Transmission sensor with overmolding and method of manufacturing the same
US8579643B2 (en) 2011-12-30 2013-11-12 Unison Industries, Llc Connector assembly and method of fabricating the same
US8970228B2 (en) * 2012-05-31 2015-03-03 General Electric Company Rotational clearance measurement system and method of operation
FR3094495B1 (en) * 2019-03-25 2021-03-05 Safran Aircraft Engines Rotation sensor with improved air gap adjustment
FR3109405B1 (en) * 2020-04-15 2022-08-12 Safran Aircraft Engines Turbomachine equipped with a system for measuring the speed of a rotor shaft
US11821811B2 (en) * 2022-02-04 2023-11-21 Pratt & Whitney Canada Corp. Fluid measurement system for an aircraft gas turbine engine and method for operating same
US11927104B2 (en) * 2022-06-22 2024-03-12 Honeywell International Inc. Aircraft engine sensing apparatus with insulated connection wires

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3213360A (en) * 1962-06-25 1965-10-19 K F Products Inc Electronic gauging system
US3260117A (en) * 1963-03-04 1966-07-12 Smith & Sons Ltd S Electric position detection devices
US3721968A (en) * 1972-02-02 1973-03-20 Electro Corp America Magnetic pickup
IT992864B (en) * 1972-08-22 1975-09-30 Maschf Augsburg Nuernberg Ag APPARATUS TO DETERMINE WITHOUT CONTACT EXACTLY AND CONTINUOUSLY THE TEMPERATURE OF SURFACES

Also Published As

Publication number Publication date
FR2392364A1 (en) 1978-12-22
US4196390A (en) 1980-04-01

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee